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US 11,485,833 B2Granted
Thermoplastic toughened matrix resins containing nanoparticles
AssigneeHexcel Corporation
InventorsYan Zhu, Gordon T. Emmerson
Life of this patent
Estimating the term…
Abstract
Pre-impregnated composite material (prepreg) that can be cured/molded to form aerospace composite parts. The prepreg includes carbon reinforcing fibers and an uncured resin matrix. The resin matrix includes an epoxy resin component, polyethersulfone as a toughening agent, a thermoplastic particle component, a nanoparticle component and a curing agent.
Claims14
A prepreg comprising:
- A) reinforcing fibers;
- B) an uncured resin matrix comprising:
- a) a resin component that comprises one or more epoxy resins;
- b) a thermoplastic particle component that comprises thermoplastic particles, said thermoplastic particle component being present in an amount ranging from 10 to 20 weight percent, based on the total weight of said uncured resin matrix, wherein said thermoplastic particles comprise hybrid polyamide particles and wherein each of said hybrid polyamide particles comprises a mixture of a semi-crystalline polyamide and an amorphous polyamide, said amorphous polyamide being present in an amount of from 20 to 80 weight percent, based on the total weight of said hybrid polyamide particle, and said semi-crystalline polyamide being present in an amount of from 20 to 80 weight percent, based on the total weight of said hybrid polyamide particle, and wherein said semi-crystalline polyamide and amorphous polyamide are comprised of different stereo isomeric forms of the polyamide which is the polymeric condensation product of 1,10-decane dicarboxylic acid and an amine component having the formula
- c) a thermoplastic toughening agent comprising polyethersulfone, said toughening agent being present in an amount ranging from 5 to 15 weight percent, based on the total weight of said uncured resin matrix;
- d) a nanoparticles component comprising nanoparticles, said nanoparticle component being present in an amount ranging from 10 to 30 weight percent, based on the total weight of said uncured resin matrix;
- and
- e) a curing agent.
5 more elements
A method for making a prepreg that is curable to form a composite part, said method comprising the steps of:
- A) providing reinforcing fibers comprising carbon fibers;
- and
- B) impregnating said reinforcing fibers with an uncured resin matrix wherein said uncured resin matrix comprises:
- a) a resin component that comprises one or more epoxy resins;
- b) a thermoplastic particle component that comprises thermoplastic particles, said thermoplastic particle component being present in an amount ranging from 10 to 20 weight percent, based on the total weight of said uncured resin matrix, wherein said thermoplastic particles comprise hybrid polyamide particles and wherein each of said hybrid polyamide particles comprises a mixture of a semi-crystalline polyamide and an amorphous polyamide, said amorphous polyamide being present in an amount of from 20 to 80 weight percent, based on the total weight of said hybrid polyamide particle, and said semi-crystalline polyamide being present in an amount of from 20 to 80 weight percent, based on the total weight of said hybrid polyamide particle, and wherein said semi-crystalline polyamide and amorphous polyamide are comprised of different stereo isomeric forms of the polyamide which is the polymeric condensation product of 1,10-decane dicarboxylic acid and an amine component having the formula
- c) a thermoplastic toughening agent comprising polyethersulfone, said toughening agent being present in an amount ranging from 5 to 15 weight percent, based on the total weight of said uncured resin matrix;
- d) a nanoparticles component comprising nanoparticles, said nanoparticle component being present in an amount ranging from 12 to 30 weight percent, based on the total weight of said uncured resin matrix;
- and
- e) a curing agent.
6 more elements
The method for making a prepreg according to 12 wherein said non-cross-linked particles comprise polyamide 11.
Dependencies are inferred from the claim text.